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dc.contributor.authorWeijian Zhao
dc.contributor.authorFan Zhang
dc.contributor.authorPanfeng Huang
dc.contributor.authorHao Wen
dc.contributor.authorTi Chen
dc.date.accessioned2025-08-17T22:29:09Z
dc.date.available2025-08-17T22:29:09Z
dc.date.copyright1/1/2025 12:00:00 AM
dc.date.issued2025
dc.identifier.otherJAEEEZ.ASENG-4633.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306999
dc.description.abstractA tethered autonomous docking system, which is composed of a rope winch installed at the bottom of the unmanned aerial vehicle (UAV), a quadrotor for autonomous docking, and a connected tether, can be widely used for unmanned delivery. Frequent ups and downs can be inevitable through the deployment/retrieval of the flexible tether. Although the tether offers several advantages compared with traditional UAV transportation, new control problems can arise as well. To solve this nonlinear, underactuated, and time-varying disturbance system, a complete control scheme, including the accurate trajectory tracking of the end quadrotor under a time-varying disturbance caused by tether and the coordinated control of the rope winch, is proposed in this paper. A complete dynamics model, including the terminal quadrotor and the rope winch, is derived. A new control scheme, combining active disturbance rejection control with finite time integral backstepping, is proposed to achieve the position tracking of the quadrotor under the unknown disturbance introduced by tether and environment. In the case of obtaining the real-time position and tether tension of the quadrotor, a position-based impedance control strategy was proposed to always keep the tether slightly tensioned. Theoretical proof and simulation are given to verify the designed control algorithm, which can provide good performance of tracking and antidisturbance.
dc.publisherAmerican Society of Civil Engineers
dc.titleCoordinated Control of a Tethered Autonomous Docking UAV
dc.typeJournal Article
dc.journal.volume38
dc.journal.issue1
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-4633
dc.journal.fristpage04024109-1
dc.journal.lastpage04024109-10
dc.page10
dc.treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 001
dc.contenttypeFulltext


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